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Nicolas Gourdain
Nicolas Gourdain
ISAE-SUPAERO, University of Toulouse
Verifisert e-postadresse på isae-supaero.fr
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High performance parallel computing of flows in complex geometries: I. methods
N Gourdain, L Gicquel, M Montagnac, O Vermorel, M Gazaix, ...
Computational Science & Discovery 2 (1), 015003, 2009
199*2009
Effects of free-stream turbulence on high pressure turbine blade heat transfer predicted by structured and unstructured LES
EC Morata, N Gourdain, F Duchaine, LYM Gicquel
International Journal of Heat and Mass Transfer 55 (21-22), 5754-5768, 2012
1232012
Large eddy simulation of flows in industrial compressors: a path from 2015 to 2035
N Gourdain, F Sicot, F Duchaine, L Gicquel
Philosophical Transactions of the Royal society A: Mathematical, Physical …, 2014
1172014
High performance parallel computing of flows in complex geometries
LYM Gicquel, N Gourdain, JF Boussuge, H Deniau, G Staffelbach, P Wolf, ...
Comptes Rendus Mécanique 339 (2-3), 104-124, 2011
1092011
Unsteady simulation of an axial compressor stage with casing and blade passive treatments
N Gourdain, F Leboeuf
1092009
Simulation of rotating stall in a whole stage of an axial compressor
N Gourdain, S Burguburu, F Leboeuf, GJ Michon
Computers & Fluids 39 (9), 1644-1655, 2010
1012010
Comparison of RANS and LES for prediction of wall heat transfer in a highly loaded turbine guide vane
N Gourdain, LYM Gicquel, E Collado
Journal of propulsion and power 28 (2), 423-433, 2012
96*2012
A time-domain harmonic balance method for rotor/stator interactions
F Sicot, G Dufour, N Gourdain
942012
Prediction of the unsteady turbulent flow in an axial compressor stage. Part 1: Comparison of unsteady RANS and LES with experiments
N Gourdain
Computers & Fluids 106, 119-129, 2015
842015
Effect of tip clearance dimensions and control of unsteady flows in a multi-stage high-pressure compressor
N Gourdain, F Wlassow, X Ottavy
832012
Numerical simulation of rotating stall in a subsonic compressor
N Gourdain, S Burguburu, F Leboeuf, H Miton
Aerospace Science and Technology 10 (1), 9-18, 2006
762006
Steady/unsteady reynolds-averaged navier–stokes and large eddy simulations of a turbine blade at high subsonic outlet mach number
T Léonard, LYM Gicquel, N Gourdain, F Duchaine
Journal of Turbomachinery 137 (4), 041001, 2015
552015
Sustainable aviation in the context of the Paris Agreement: A review of prospective scenarios and their technological mitigation levers
S Delbecq, J Fontane, N Gourdain, T Planès, F Simatos
Progress in Aerospace Sciences 141, 100920, 2023
512023
Numerical analysis of the tip leakage flow field in a transonic axial compressor with circumferential casing treatment
G Legras, N Gourdain, I Trebinjac
Journal of Thermal Science 19, 198-205, 2010
432010
Chemical kinetics modeling and LES combustion model effects on a perfectly premixed burner
G Albouze, T Poinsot, L Gicquel
Comptes Rendus Mécanique 337 (6-7), 318-328, 2009
422009
Experimental and computational methods for flow investigation in high-speed multistage compressor
X Ottavy, N Courtiade, N Gourdain
Journal of propulsion and power 28 (6), 1141-1155, 2012
412012
Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on its test-rig—part I: rotating stall
F Crevel, N Gourdain, S Moreau
Journal of Turbomachinery 136 (10), 101003, 2014
382014
Towards massively parallel large eddy simulation of turbine stages
G Wang, D Papadogiannis, F Duchaine, N Gourdain, LYM Gicquel
Turbo Expo: Power for Land, Sea, and Air 55249, V06CT42A021, 2013
352013
Simulation numérique des phénomènes de décollement tournant dans les compresseurs axiaux
N Gourdain
Ecully, Ecole centrale de Lyon, 2005
322005
Prediction of the unsteady turbulent flow in an axial compressor stage. Part 2: Analysis of unsteady RANS and LES data
N Gourdain
Computers & Fluids 106, 67-78, 2015
312015
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Artikler 1–20